scope:

This Part 4 of the spacecraft thermal control and design data handbooks, provides information on calculating the conductive heat transfer rate for a variety of two and three-dimensional configurations.

Calculations for the conductance of the interface between two surfaces (joints) require special consideration and are included as a separate clause.

The Thermal design handbook is published in 16 Parts

TR 17603-31-01 Thermal design handbook - Part 1: View factors

TR 17603-31-02 Thermal design handbook - Part 2: Holes, Grooves and Cavities

TR 17603-31-03 Thermal design handbook - Part 3: Spacecraft Surface Temperature

TR 17603-31-04 Thermal design handbook - Part 4: Conductive Heat Transfer

TR 17603-31-05 Thermal design handbook - Part 5: Structural Materials: Metallic and Composite

TR 17603-31-06 Thermal design handbook - Part 6: Thermal Control Surfaces

TR 17603-31-07 Thermal design handbook - Part 7: Insulations

TR 17603-31-08 Thermal design handbook - Part 8: Heat Pipes

TR 17603-31-09 Thermal design handbook - Part 9: Radiators

TR 17603-31-10 Thermal design handbook - Part 10: Phase - Change Capacitors

TR 17603-31-11 Thermal design handbook - Part 11: Electrical Heating

TR 17603-31-12 Thermal design handbook - Part 12: Louvers

TR 17603-31-13 Thermal design handbook - Part 13: Fluid Loops

TR 17603-31-14 Thermal design handbook - Part 14: Cryogenic Cooling

TR 17603-31-15 Thermal design handbook - Part 15: Existing Satellites

TR 17603-31-16 Thermal design handbook - Part 16: Thermal Protection System